TY - GEN
T1 - Analysis and design of three loop radar servo system for air defense missile
AU - Li, Fugui
AU - Xia, Qunli
AU - Qi, Zaikang
PY - 2011
Y1 - 2011
N2 - In order to design a radar servo system with satisfactory response for an air defense missile, the three loop form was chosen, and the frequency domain method was used. The design approach and criteria for the three loop radar servo system was outlined in this paper. With the criteria, a servo system was designed. Then the effect of every loop was analyzed. The results shows that, with the frequency domain method and the design criteria, the designed radar servo system can obtain good response and every loop of the three loop form can't be omitted due to their essential effect.
AB - In order to design a radar servo system with satisfactory response for an air defense missile, the three loop form was chosen, and the frequency domain method was used. The design approach and criteria for the three loop radar servo system was outlined in this paper. With the criteria, a servo system was designed. Then the effect of every loop was analyzed. The results shows that, with the frequency domain method and the design criteria, the designed radar servo system can obtain good response and every loop of the three loop form can't be omitted due to their essential effect.
KW - Design criteria
KW - Effect analysis
KW - Frequency domain method
KW - Radar servo system
KW - Three loop form
UR - http://www.scopus.com/inward/record.url?scp=79952851316&partnerID=8YFLogxK
U2 - 10.1109/ICMTMA.2011.114
DO - 10.1109/ICMTMA.2011.114
M3 - Conference contribution
AN - SCOPUS:79952851316
SN - 9780769542966
T3 - Proceedings - 3rd International Conference on Measuring Technology and Mechatronics Automation, ICMTMA 2011
SP - 451
EP - 454
BT - Proceedings - 3rd International Conference on Measuring Technology and Mechatronics Automation, ICMTMA 2011
T2 - 3rd International Conference on Measuring Technology and Mechatronics Automation, ICMTMA 2011
Y2 - 6 January 2011 through 7 January 2011
ER -